Fatigue Life Prediction Based on Crack Closure and Equivalent Initial Flaw Size
Author:
Funder
National Natural Science Foundation of China
Publisher
MDPI AG
Subject
General Materials Science
Link
http://www.mdpi.com/1996-1944/8/10/5367/pdf
Reference51 articles.
1. Application of local stress–strain approaches in the prediction of fatigue crack initiation life for cyclically non-stabilized and non-Masing steel
2. A Damage Tolerance Method for Helicopter Dynamic Components
3. Determination of fatigue related discontinuity state of 7000 series of aerospace aluminum alloys
4. Probabilistic fatigue life prediction using an equivalent initial flaw size distribution
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